公开(公告)号：US20180010795A1

公开(公告)日：2018-01-11

申请号：US15202751

申请日：2016-07-06

Applicant: General Electric Company

Inventor： Hiranya Kumar Nath ,  Manampathy Gangadharan Giridharan

IPC: F23R3/00

CPC classification number: F23R3/002 ,  F23R3/18 ,  F23R3/286 ,  F23R3/50

Abstract: A deflector for a gas turbine engine combustor. The combustor includes a liner defining a combustion zone and a mixer assembly configured to supply the combustion zone with a predetermined mixture of fuel and air. The deflector includes a deflector body configured to couple to the liner. The deflector body includes a first surface configured to reflect thermal radiation to a predetermined focal area, and an aperture extending through the deflector body and configured to receive the mixer assembly therethrough.